JP2015535565A - タービンシュラウドの取り付け及び封止の構成 - Google Patents

タービンシュラウドの取り付け及び封止の構成 Download PDF

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Publication number
JP2015535565A
JP2015535565A JP2015543049A JP2015543049A JP2015535565A JP 2015535565 A JP2015535565 A JP 2015535565A JP 2015543049 A JP2015543049 A JP 2015543049A JP 2015543049 A JP2015543049 A JP 2015543049A JP 2015535565 A JP2015535565 A JP 2015535565A
Authority
JP
Japan
Prior art keywords
shroud
turbine
casing
seal member
shroud segment
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2015543049A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015535565A5 (pt
Inventor
アルバース，ジョゼフ・チャールズ
プロクター，ロバート
シェルトン，モンティ・リー
ルッソ，リチャード，ジュニア
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2015535565A publication Critical patent/JP2015535565A/ja
Publication of JP2015535565A5 publication Critical patent/JP2015535565A5/ja
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2015543049A 2012-11-21 2013-10-15 タービンシュラウドの取り付け及び封止の構成 Pending JP2015535565A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/683,813 2012-11-21
US13/683,813 US9238977B2 (en) 2012-11-21 2012-11-21 Turbine shroud mounting and sealing arrangement
PCT/US2013/064916 WO2014081517A1 (en) 2012-11-21 2013-10-15 Turbine shroud mounting and sealing arrangement

Publications (2)

Publication Number Publication Date
JP2015535565A true JP2015535565A (ja) 2015-12-14
JP2015535565A5 JP2015535565A5 (pt) 2016-12-01

Family

ID=49943492

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015543049A Pending JP2015535565A (ja) 2012-11-21 2013-10-15 タービンシュラウドの取り付け及び封止の構成

Country Status (7)

Country Link
US (1) US9238977B2 (pt)
EP (1) EP2923041A1 (pt)
JP (1) JP2015535565A (pt)
CN (1) CN104797784B (pt)
BR (1) BR112015010425A2 (pt)
CA (1) CA2891616A1 (pt)
WO (1) WO2014081517A1 (pt)

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* Cited by examiner, † Cited by third party
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EP2696037B1 (de) * 2012-08-09 2017-03-01 MTU Aero Engines AG Abdichtung des Strömungskanals einer Strömungsmaschine
US10612407B2 (en) 2013-02-28 2020-04-07 United Technologies Corporation Contoured blade outer air seal for a gas turbine engine
US20140271142A1 (en) 2013-03-14 2014-09-18 General Electric Company Turbine Shroud with Spline Seal
JP6233578B2 (ja) * 2013-12-05 2017-11-22 株式会社Ihi タービン
EP3228826B1 (de) * 2016-04-05 2021-03-17 MTU Aero Engines GmbH Dichtungssegmentanordnung mit steckverbindung, zugehörige gasturbine und herstellungsverfahren
US20180340437A1 (en) * 2017-02-24 2018-11-29 General Electric Company Spline for a turbine engine
US20180355754A1 (en) * 2017-02-24 2018-12-13 General Electric Company Spline for a turbine engine
US10648362B2 (en) * 2017-02-24 2020-05-12 General Electric Company Spline for a turbine engine
US10655495B2 (en) * 2017-02-24 2020-05-19 General Electric Company Spline for a turbine engine
US20180347399A1 (en) * 2017-06-01 2018-12-06 Pratt & Whitney Canada Corp. Turbine shroud with integrated heat shield
US10519790B2 (en) * 2017-06-15 2019-12-31 General Electric Company Turbine shroud assembly
FR3071273B1 (fr) * 2017-09-21 2019-08-30 Safran Aircraft Engines Ensemble d'etancheite de turbine pour turbomachine
US10982559B2 (en) * 2018-08-24 2021-04-20 General Electric Company Spline seal with cooling features for turbine engines
US20200141276A1 (en) * 2018-11-07 2020-05-07 General Electric Company Turbine shroud with lapped seal segments
FR3096723B1 (fr) * 2019-05-29 2022-03-25 Safran Helicopter Engines Anneau d’etancheite pour une roue de turbine de turbomachine
FR3100838B1 (fr) * 2019-09-13 2021-10-01 Safran Aircraft Engines Anneau d’etancheite de turbomachine
US11608752B2 (en) 2021-02-22 2023-03-21 General Electric Company Sealing apparatus for an axial flow turbomachine
CN115263808B (zh) * 2022-09-28 2023-02-21 中国航发四川燃气涡轮研究院 集成式双转子航空发动机的中介机匣

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05240066A (ja) * 1991-11-27 1993-09-17 General Electric Co <Ge> タービンシュラウド、タービンシュラウドセグメント及びガスタービンエンジン用のタービン
JP2005030315A (ja) * 2003-07-04 2005-02-03 Ishikawajima Harima Heavy Ind Co Ltd シュラウドセグメント
JP2011252440A (ja) * 2010-06-02 2011-12-15 Mitsubishi Heavy Ind Ltd ハニカム部材の温度推定方法及びハニカム部材

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GB2081817B (en) 1980-08-08 1984-02-15 Rolls Royce Turbine blade shrouding
US4512712A (en) 1983-08-01 1985-04-23 United Technologies Corporation Turbine stator assembly
GB2206651B (en) 1987-07-01 1991-05-08 Rolls Royce Plc Turbine blade shroud structure
GB2249356B (en) 1990-11-01 1995-01-18 Rolls Royce Plc Shroud liners
US5232340A (en) 1992-09-28 1993-08-03 General Electric Company Gas turbine engine stator assembly
US5927942A (en) 1993-10-27 1999-07-27 United Technologies Corporation Mounting and sealing arrangement for a turbine shroud segment
US5738490A (en) 1996-05-20 1998-04-14 Pratt & Whitney Canada, Inc. Gas turbine engine shroud seals
EP0844369B1 (en) 1996-11-23 2002-01-30 ROLLS-ROYCE plc A bladed rotor and surround assembly
US6120242A (en) 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
US6341938B1 (en) 2000-03-10 2002-01-29 General Electric Company Methods and apparatus for minimizing thermal gradients within turbine shrouds
US6340285B1 (en) 2000-06-08 2002-01-22 General Electric Company End rail cooling for combined high and low pressure turbine shroud
US6902371B2 (en) * 2002-07-26 2005-06-07 General Electric Company Internal low pressure turbine case cooling
US6814538B2 (en) 2003-01-22 2004-11-09 General Electric Company Turbine stage one shroud configuration and method for service enhancement
US7186078B2 (en) * 2003-07-04 2007-03-06 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbine shroud segment
JP4285134B2 (ja) 2003-07-04 2009-06-24 株式会社Ｉｈｉ シュラウドセグメント
US7147429B2 (en) 2004-09-16 2006-12-12 General Electric Company Turbine assembly and turbine shroud therefor
US7377742B2 (en) 2005-10-14 2008-05-27 General Electric Company Turbine shroud assembly and method for assembling a gas turbine engine
FR2899275A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine
US7527477B2 (en) 2006-07-31 2009-05-05 General Electric Company Rotor blade and method of fabricating same
US8240985B2 (en) 2008-04-29 2012-08-14 Pratt & Whitney Canada Corp. Shroud segment arrangement for gas turbine engines
JP5384983B2 (ja) 2009-03-27 2014-01-08 本田技研工業株式会社 タービンシュラウド
US8740552B2 (en) 2010-05-28 2014-06-03 General Electric Company Low-ductility turbine shroud and mounting apparatus
US8753073B2 (en) 2010-06-23 2014-06-17 General Electric Company Turbine shroud sealing apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05240066A (ja) * 1991-11-27 1993-09-17 General Electric Co <Ge> タービンシュラウド、タービンシュラウドセグメント及びガスタービンエンジン用のタービン
JP2005030315A (ja) * 2003-07-04 2005-02-03 Ishikawajima Harima Heavy Ind Co Ltd シュラウドセグメント
JP2011252440A (ja) * 2010-06-02 2011-12-15 Mitsubishi Heavy Ind Ltd ハニカム部材の温度推定方法及びハニカム部材

Also Published As

Publication number Publication date
CN104797784B (zh) 2016-09-14
WO2014081517A1 (en) 2014-05-30
EP2923041A1 (en) 2015-09-30
BR112015010425A2 (pt) 2018-04-10
CA2891616A1 (en) 2014-05-30
US9238977B2 (en) 2016-01-19
CN104797784A (zh) 2015-07-22
US20140140833A1 (en) 2014-05-22

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